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Figure 1A
DOT Approved
Sep 25/90
44,600
MODEL CL-600-2A12
AIRPLANE FLIGHT MANUAL
PSP 601-1A-1
THIS PAGE INTENTIONALLY LEFT BLANK
DOT Approved
Sf 25/90 LIMITATIONS
44,600 Page 4A
MODEL CL-600-2A12
AIRPLANE FLIGHT MANUAL
PSP 601-1A-1
3. OPERATING LIMITATIONS
A. TYPES OF OPERATION
This airplane is certificated in the transport category and is eligible
for the following kinds of operations when the appropriate instruments
and equipment required by the airworthiness and/or operating certificate
are installed and approved and are in operable condition.
Day and night
VFR
IFR
Icing conditions
On airplanes incorporating Canadair Service Bulletin 601-0484, Reduced
Vertical Separation Minimum (RVSM) - 1000 Ft. Aircraft Qualification
Requirements:
This airplane is certificated capable of RVSM operations in accordance
with FAA "Interim guidance material on the approval of operations/
aircraft for RVSM operations", 91-RVSM, dated March 14, 1994.
NOTE
Compliance with the standard noted above does
not constitute RVSM operational approval.
B. ALTITUDE AND TEMPERATURE OPERATING LIMITS
Maximum airport pressure altitude for take-off and landing is
10,000 feet.
Maximum operating altitude is 41,000 feet.
Maximum air temperature approved for take-off and landing is ISA +35°C
(+50°C (122°F)).
Minimum temperature approved for take-off is -40°C (-40°F).
When the ambient temperature is -30°C (-22°F) or below, the engines must
be motored for 60 seconds and the fan must rotate before engine start is
initiated.
C. RUNWAY SURFACE
Both igniters on both engines must be on continuously for take-off and
landing on runway surfaces covered with standing water, slush or snow or
in icing conditions.
DOT Approved
LIMITATIONS fl Mar 27/97
Page 4B 44,600/45,100
nr
MODEL CL-600-2A12
AIRPLANE FUGHT MANUAL
PSP 601-1A-1
TAHEO.
UllDffllG UMBS
-80- -fe-
AMBIENT ERATURE
v—'—r l—'—nr
•100 -80 -60 -40 -20 0 20 40 60 80 100 120 140
AMBIENT TEMPERATURE - °F
DOT Approved
Oct 28/96
44,600/45,100
Altitude and Temperature Operating Limits
Figure 2 LIMITATIONS
Page 5
canadair
chanenqer
MODEL CL-600-2A12
AIRPLANE FLIGHT MANUAL
PSP 601-1A-1
3. OPERATING LIMITATIONS (Cont'd)
D. RUNWAY SLOPES
The maximum runway slopes approved for take-off and landing are:
+2% (uphill)
-2% (downhill)
E. TAILWIND CONDITIONS
The maximum tail wind component approved for take-off and landing is 10
knots.
F. MINIMUM FLIGHT CREW
The minimum flight crew is one pilot and one copilot.
G. MAXIMUM OCCUPANTS
The total number of occupants, including no more than nineteen passengers,
must not exceed the lesser of the following:
(1) Twenty-two or,
(2) The number for which seating accomodation approved for take-off and
landing is provided.
DOT Approved
LIMITATIONS Apr 21/03
Page 6 44,600/45,100
canadair
chanenqer
MODEL CL-600-2A12
AIRPLANE FLIGHT MANUAL
PSP 601-1A-1
3. OPERATING LIMITATIONS (Cont'd)
H. OPERATION IN ICING CONDITIONS
During cold weather operations, the flight crew must ensure that the
airplane fuselage, wings and tail surfaces are free from ice, snow or
frost.
(1) Cowl Anti-ice System
(a) Ground Operations
The engine cowl anti-ice system must be on when the OAT is 10°C
(50°F) or below and visible moisture in any form is present
(such as fog with visibility of one mile or less, rain, snow,
sleet and ice crystals).
The engine cowl anti-ice system must also be on when the OAT is
10°C (50°F) or below when operating on runways, ramps, or
taxi ways where surface snow, ice, standing water or slush is
present.
(b) Flight Operations
NOTE
Icing conditions exist in flight at a TAT of
10°C (50°F) or below and visible moisture in
any form is encountered (such as clouds,
rain, snow, sleet or ice crystals), except
when the SAT is -40°C (-40°F) or below.
The engine cowl anti-ice system must be on:
At or above 22,000 feet:
• when ice is indicated by the ice detection system, or
• when in icing conditions, if an ice detector has failed.
Below 22,000 feet:
• when in icing conditions, or
• when ice is indicated by the ice detection system.
DOT Approved
Apr 21/03 LIMITATIONS
44,600/45,100 Page 6A
canadair
chanenqer
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